2009 AGUSTA AW109 Grand SOLD

Avionics Copilot flight/navigation instruments (LCD EADI and EHSI, barometric altimeter, airspeed indicator, VSI) Gyrocompass C14 Honeywell Vertical gyro #1 46060-11 Flightline System Vertical gyro #2 VG-208 JET Electronics 3-axis duplex AFCS SP711 Honeywell ADF KR 87 Bendix/King Transponder (mode S) KT 73 Bendix/King VHF#1 COM/NAV/GPS GNS 530 Garmin VHF#2 COM/NAV/GPS GNS 430 Garmin DME KDM 706A Bendix/King Marker beacon KMR 675 Bendix/King Pilot ICS (including pilot/copilot control panel. mode controller. audio cabin control) AC power supply system (two inverters) Copilot flight/navigation instruments (LCD EADI and EHSI. barometric altimeter airspeed indicator. VSI) Flight director FZ 702 Honeywell with autotrim Radio altimeter AA 300 Honeywell ELT C406-2HM Artex Moving map KMD 550 Bendix/King Radio master switch with ground function EFIS pilot/copilot in command switch Moving Map MKII Observer (Sky Force) TCAS SKY 791 (BF Goodrich) Weather Radar presented on pilot/copilot EHSI RDR 2000 Bendix/King. Two (2) independent electronic control systems (FADEC) w/ emergency training operation modes auto start Airspeed indicator Instantaneous vertical speed indicator Barometric encoding altimeter Magnetic compass indicator Clock. 8 days and elapsed time LC Integrated Display System (IDS) Master Warning Caution lights Engine fire detection system Aural Warning Generator system Exceedance recorder system (on IDS display) Interior Soundproofing PAULSTRA VIP Interior (5 places) including leatherette covered or painted liners. 3 seats aft facing central bench and see-through with foldable armrest and 2 seats aft bench fwd facing with central cabinet/bar. Additional amenities include advisory, reading and floor courtesy light, Floor carpeting, Cabin double glass windows, Two individual crash-resistant pilot seats fore and aft adjustable with lap belts, Aluminium alloy honeycomb reinforced floor with anti-skid finishing, Ventilation ram air inlets, passive vibration absorber Exterior Beige paint scheme with dark stripes Additional Equipment Air conditioning ECU Garret Emergency floats provision Structural provision for utility equipment (emergency floats, rescue hoist, cargo hook) Reinforced windshield 213 US gall. Fuel system Baggage compartment extension (to 1.9 m) Engine compartment fire extinguishers Baggage compartment extension (2,3 mt) Baggage compartment light Pilot and copilot shoulder harness with inertia reel Crew open door actuators Quick disconnecting chip detectors Pulsed chip detector Fuel drain electrical valves Tail boom strake Airframe hour meter provision Dual control Rotor brake 450 W Retractable/Rotating landing light Pilot and copilot windshield wipers Wiper switch on pilot cyclic grip Rotorcraft Flight Manual and technical publications Hook for Jacket (nr. 2) right and left in pax cabin Locking fuel cap Ground fuel drains Airframe mounted easy access fuel filter Engine oil chip detectors (one per engine) Two independent fuel systems with cross-feeding valve and control panel 3-cell crash-resistant fuel system (460 kg – 152 USG) Submerged fuel boost pump (one per system) RH refueling point High-intensity strobe lights on horizontal stabilizer Ground tools kit (including tow bar. lifting tool. wheel chocks) Air intake/exhaust covers Pitot tubes covers Tie-down fittings Portable fire extinguisher First aid kit Fuel cup with key-lock Six (6) Active Noise Reduction (ANR) headsets